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25 February 1997, Volume 18 Issue 1

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25 February 1997, Volume 18 Issue 1

LOAD SPECTRUM DRAWING FOR THE ACCELERATIVE TEST OF THE AIRCRAFT COMPONENT AND THE DAMAGE PROBABILITY DISTRIBUTION
Abstract( 1920 )

Xiong Junjiang;Gao Zhentong;Yan Chuliang;Meng Fanpei

1997, (1): 1-5.

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ANALYSIS OF DYNAMIC QUALITY FOR MANEUVERING TARGET TRACKING FIRE CONTROL INTEGRATED SYSTEM
Abstract( 2235 )

Xu Xizheng;Jing Zhongliang;Jin Dekun;Zhu Gehao

1997, (1): 6-11.

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COMPLEX DYNAMIC SYSTEM FAILURE DETECTION AND DIAGNOSIS
Abstract( 2304 )

Ge Tong;Deng Jianhua

1997, (1): 12-16.

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EFFECT OF FLIGHT CONTROL SYSTEM ON PILOT INDUCED OSCILLATION
Abstract( 2161 )

Wang Yongxi

1997, (1): 17-21.

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KEY TECHNOLOGY IN THE DEVELOPMENT OF HIGH PERFORMANCE DYNAMIC AIRLOAD SIMULATION SYSTEM
Abstract( 1905 )

Yan Jie;Sun Li;Yang Jun;Yu Yunfeng

1997, (1): 22-25.

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SUPERMANEUVERABLE FLIGHT CONTROL USING DYNAMICA INVERSION BASED NEURAL NETWORKS
Abstract( 2243 )

Liu Shuxiang;Guo Suofeng;Xu Xiaohao

1997, (1): 26-30.

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GALVANIC CORROSION OF HIGH STRENGTH ALUMINUM ALLOYS IN THE SOLUTION SIMULATING THE AIRCRAFT CORROSION ENVIRONMENT
Abstract( 1649 )

Zhu Liqun;Li Weiping;Zhang Qi;Li Di;Zhang Yumei

1997, (1): 31-36.

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NUMERICAL SIMULATION OF DIRECT AGED FORGING PROCESS OF GH4169 ALLOY
Abstract( 1615 )

Liu Dong;Luo Zijian

1997, (1): 37-43.

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ON THE STRENGTHENING MECHANISM OF HIGH Co Ni ULTRAHIGH STRENGTH STEEL
Abstract( 1473 )

Ling Bin;Zhong Ping;Zhong Bingwen;Zhao Zhengye;Zhang Shaoqing

1997, (1): 44-49.

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POSITION CONSTRAINT PARAMETERIZATION IN FEATURE BASED DESIGN
Abstract( 1322 )

Yang Yunping;Zhou Rurong;Ye Shanghui

1997, (1): 50-56.

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INTERFACIAL STABILITY AND SELF SCALING BEHAVIOR OF A NEW MULTI LAYER GH220/Ti N CoCrAlTaY/Al PROTECTIVE COATING
Abstract( 1455 )

Wang Jiajun;Yang Zhigang;Li Chunming;Zheng Yankang

1997, (1): 57-61.

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GENERATION OF 3 D MUTLI BLOCKED STRUCTURE BODY FITTED GRIDS OF A COMPLEX CONFIGURATION FLYING BODY
Abstract( 2621 )

Zhu Junzheng;Fan Xijun

1997, (1): 62-66.

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A FURTHER INVESTIGATION ON THE SOUND SPEED IN GAS LIQUID TWO PHASE FLOW
Abstract( 2203 )

Wang Yongqing;Deng Xinjian;Yu Chengye

1997, (1): 67-70.

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STUDY OF THE THICKNESS NOISE OF HELICOPTER ROTORS BASED ON THE COLLAPSING SPHERE METHOD
Abstract( 2074 )

Qiao Weiyang;Tang Diyi;Li Wenlan

1997, (1): 71-74.

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NEW METHOD FOR OBTAINING SONIC FATIGUE S N CURVES AT ELEVATED TEMPERATURE
Abstract( 2100 )

Ge sen;Cao Qi;Shao Chuang;Guo Dingwen

1997, (1): 75-77.

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VECTOR SPACE AND ITS RESOLUTION IN PROPULSION SYSTEM′S MATHEMATICAL MODEL
Abstract( 1890 )

Shan Peng

1997, (1): 78-82.

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SIMPLIFIED PROBABILISTIC DATA ASSOCIATION ALGORITHM
Abstract( 1969 )

Li Jianxun;Jing Zhongliang;Dai Guanzhong;Jin Dekun

1997, (1): 83-85.

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INTELLEGENT FAULT TOLERANCE CONTROLLER FOR SERVO MOTOR OF PLATFORM IN AN INERTIAL NAVIGATION SYSTEM
Abstract( 2344 )

Yan Lei;Wang Lina;Fan Yuezu;Zhang Hongyue

1997, (1): 86-88.

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PREPROCESSING FOR ISAR MOTION COMPENSATION AND IMAGING IN THE CORSS RANGE
Abstract( 2204 )

She Zhishun;Zhu Zhaoda

1997, (1): 89-92.

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THE CUTOFF WAVELENGTH AND APPROXIMATE SOLVED FIELDS OF A CAM RECTANGULAR WAVEGUIDE
Abstract( 2341 )

Lü Shanwei;Chen Gang;Gao Wenjun

1997, (1): 93-95.

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THE DEVELOPMENT OF A RAM AIR DRIVEN ENVIRONMENTAL CONTROL SYSTEM FOR AVIONICS PODS
Abstract( 1847 )

Yu Jianzu;Qian Yiji

1997, (1): 96-99.

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STUDIES ON THE TECHNOLOGY OF ACTIVE VIBRATION CONTROL BY USING PIEZOELECTRIC ACTUATORS
Abstract( 1383 )

Mei Shengmin;Tao Baoqi;Qin Taiyan

1997, (1): 100-103.

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MODEL REDUCTION FOR LARGE SPACE STRUCTURAL SYSTEMS VIA GENETIC ALGORITHMS
Abstract( 1333 )

Chen Genshe;Wen Chuanyuan;Li Bijiang

1997, (1): 104-107.

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DISCUSSION ON OBJECTIVE FUNCTIONS FOR OPTIMUM DESIGN OF LOW RCS AIRCRAFT COMFIGURATION
Abstract( 1212 )

Yu Xiongqing;Yang Jingzhuo

1997, (1): 108-111.

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NONLINEAR INVERSION DYNAMIC NEUROCONTROL METHOD FOR FLIGHT DECOUPLING CONTROL PROBLEMS
Abstract( 1065 )

Ruan Xiaogang Guo Suofeng

1997, (1): 112-116.

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CONTROL SYSTEM OF SEMI DIFFERENTIAL YAWING FOR COAXIAL HELICOPTERS
Abstract( 1364 )

Feng Yachang;Du Huifang

1997, (1): 117-119.

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SENSOR FUSION VIA NEURAL NETWORKS FOR ESTIMATION OF TOOL WEAR
Abstract( 1112 )

Zhu Mingquan;Cai Yongxia

1997, (1): 120-122.

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MICROSTRUCTURE AND STABILITY OF SILICON CARBIDE CHEMICAL VAPOR DEPOSITED AT NORMAL ATMOSPHERE PRESSURE
Abstract( 1394 )

Xu Yongdong;Zhang Litong;Cheng Laifei

1997, (1): 123-126.

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VISUALIZED DESIGN SYSTEM FOR PARALLEL PROGRAMS
Abstract( 985 )

Cai Hua

1997, (1): 127-127.

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